.jpg "MS-14VM Turboshaft engine © Konstantinos Panitsidis")
Photo from the personal collection of Konstantinos Panitsidis
Technical specifications 
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Designers: Motor Sich, JSC Zaporozhye, Ukraine
Manufacturer: Motor Sich, JSC Zaporozhye, Ukraine
The MS-14VM engine is a turboshaft version of the MS-14 engine. The engine can be used as a power plant for medium-class helicopters and for retrofitting of Mi-8T helicopters.
TECHNICAL SPECIFICATIONS
| Fuel | - |
| Oil | - |
| Propeller shaft power, take-off power rating | 1.600 h.p. |
| Specific fuel consumption, take-off power rating | 0,240 kg/e.h.p.* h |
| Propeller shaft power, cruise power (H=0.0 m, M=0.0, ISA +25oC) | 1.100 h.p. |
| Specific fuel consumption, cruise power | 0,265 kg/e.h.p.* h |
| Pressure ratio, take-take-off power rating | - |
| Temperature of the gas at the turbine intake, take-off power rating | - |
| Air flow rate, take-off power rating | - |
| Compressor rotation frequency low-pressure, take-off power rating | - |
| Diameter | - |
| Height | - |
| Width | - |
| Lenght | - |
| Weight | 310+10 kg |
| Specified service life | - |
